Search results for query: *

Just to assist anyone who is willing to provide assistance, here I attached the input file. What I wanted is the interlaminar shear stress at the top and bottom surface of the core, specifically between the layer of top/bottom plate and the core. Please provide me the correct interlaminar shear...

Hi, I'm currently modeling a 3 layers sandwich panel (2400 x 1500 mm). My task is to get the interlaminar shear stress value at the top surface and bottom surface of the core. I'm using SHELL181 element and I assign top layer thickness to be 11 mm, core thickness to be 68 mm and bottom layer...

Hi, I'm currently modeling a 3 layers sandwich panel (2400 x 1500 mm). My task is to get the interlaminar shear stress value at the top surface and bottom surface of the core. I'm using SHELL181 element and I assign top layer thickness to be 11 mm, core thickness to be 68 mm and bottom layer...

Hi. I do not know what boundary supports should I use on icebreaker hull model. All I know is I have to apply an ice pressure on the tip of the bottom of the bow. However, I still need the supports to constraint the model in order for the non linear analysis to work properly. So, what type of...

Thank you for your replies. I'm still new in composite analysis and trying to learn as much. Another thing, is there any specific value or range of values of interlaminar shear stress than can cause failure in sandwich laminates?

Wow RP thank you so much, same goes to SW. Those links really help a lot ! "For an actual structure you need to do structual analysis to assess the shear/unit width, and then apply the shear stress formula as we've described. For a simply supported flat rectangular plate the peak will be in...

bump ! The thickness of the top and bottom plates is 4 mm and the core is 20 mm. The top and bottom plates are made of steel and the core is made of elastomer. I need to know the correct procedure to determine interlaminar shear stress due to uniformly distributed load which is applied in normal...

Hi. I'm having trouble to determine interlaminar shear stress in sandwich plate laminates. Does anyone has a procedure or program to calculate interlaminar shear stress in sandwich plate of 3 layer?